Arlington, TX, United States of America

John V Howard



Average Co-Inventor Count = 2.7

ph-index = 4

Forward Citations = 81(Granted Patents)


Company Filing History:


Years Active: 1982-2011

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5 patents (USPTO):Explore Patents

Title: Innovations of John V Howard

Introduction

John V Howard is a notable inventor based in Arlington, TX (US), recognized for his contributions to the field of aerospace engineering. He holds a total of 5 patents, showcasing his innovative spirit and technical expertise.

Latest Patents

One of his latest patents is the "Torsionally De-coupled Engine Mount System." This invention is designed for tilt rotor aircraft applications, where an engine is mounted at its forward end to a prop rotor gear box using a simple adapter fitting. At its aft end, the engine connects to a pylon assembly through a bi-pod fitting. The forward mount effectively counteracts forces and moments in six degrees of freedom, while the aft mount addresses only lateral and vertical loads. This innovative system allows for tuning the engine's contribution to the overall dynamic response of the aircraft by adjusting the size, shape, weight, and material of the forward mount. The torsionally de-coupled engine mount system prevents rotor torque from being induced into the engines, enhancing the aircraft's performance.

Career Highlights

Throughout his career, John V Howard has worked with prominent companies in the aerospace sector, including Bell Helicopter Textron Inc. and Textron Corporation. His experience in these organizations has significantly contributed to his development as an inventor.

Collaborations

John has collaborated with notable professionals in the industry, including Ramesh Thiagarajan and Michael Reaugh Smith. These partnerships have fostered innovation and advancement in aerospace technologies.

Conclusion

John V Howard's contributions to aerospace engineering, particularly through his innovative patents, have made a significant impact in the field. His work continues to influence the design and functionality of tilt rotor aircraft systems.

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